/**************************************************************************** * * Copyright (c) 2012-2015 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions * are met: * * 1. Redistributions of source code must retain the above copyright * notice, this list of conditions and the following disclaimer. * 2. Redistributions in binary form must reproduce the above copyright * notice, this list of conditions and the following disclaimer in * the documentation and/or other materials provided with the * distribution. * 3. Neither the name PX4 nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE * POSSIBILITY OF SUCH DAMAGE. * ****************************************************************************/ /** * @file PreflightCheck.cpp * * Preflight check for main system components * * @author Lorenz Meier * @author Johan Jansen */ #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include "PreflightCheck.h" namespace Commander { static bool magnometerCheck(int mavlink_fd) { int fd = open(MAG0_DEVICE_PATH, 0); if (fd < 0) { warn("failed to open magnetometer - start with 'hmc5883 start' or 'lsm303d start'"); mavlink_log_critical(mavlink_fd, "SENSOR FAIL: NO MAG"); return false; } int calibration_devid; int devid = ioctl(fd, DEVIOCGDEVICEID,0); param_get(param_find("CAL_MAG0_ID"), &(calibration_devid)); if (devid != calibration_devid){ warnx("magnetometer calibration is for a different device - calibrate magnetometer first (dev: %d vs cal: %d)", devid, calibration_devid); mavlink_log_critical(mavlink_fd, "SENSOR FAIL: MAG CAL ID"); return false; } int ret = ioctl(fd, MAGIOCSELFTEST, 0); if (ret != OK) { warnx("magnetometer calibration missing or bad - calibrate magnetometer first"); mavlink_log_critical(mavlink_fd, "SENSOR FAIL: MAG CHECK/CAL"); return false; } close(fd); return true; } static bool accelerometerCheck(int mavlink_fd) { int fd = open(ACCEL0_DEVICE_PATH, O_RDONLY); int ret = ioctl(fd, ACCELIOCSELFTEST, 0); int calibration_devid; int devid = ioctl(fd, DEVIOCGDEVICEID,0); param_get(param_find("CAL_ACC0_ID"), &(calibration_devid)); if (devid != calibration_devid){ warnx("accelerometer calibration is for a different device - calibrate accelerometer first"); mavlink_log_critical(mavlink_fd, "SENSOR FAIL: ACC CAL ID"); return false; } if (ret != OK) { warnx("accel self test failed"); mavlink_log_critical(mavlink_fd, "SENSOR FAIL: ACCEL CHECK/CAL"); return false; } // check measurement result range struct accel_report acc; ret = read(fd, &acc, sizeof(acc)); if (ret == sizeof(acc)) { // evaluate values float accel_magnitude = sqrtf(acc.x * acc.x + acc.y * acc.y + acc.z * acc.z); // evaluate values if (accel_magnitude > 30.0f) { //m/s^2 warnx("accel with spurious values"); mavlink_log_critical(mavlink_fd, "SENSOR FAIL: |ACCEL| > 30 m/s^2"); //this is frickin' fatal return false; } } else { warnx("accel read failed"); mavlink_log_critical(mavlink_fd, "SENSOR FAIL: ACCEL READ"); //this is frickin' fatal return false; } close(fd); return true; } static bool gyroCheck(int mavlink_fd) { int fd = open(GYRO0_DEVICE_PATH, 0); int calibration_devid; int devid = ioctl(fd, DEVIOCGDEVICEID,0); param_get(param_find("CAL_GYRO0_ID"), &(calibration_devid)); if (devid != calibration_devid){ warnx("gyro calibration is for a different device - calibrate gyro first"); mavlink_log_critical(mavlink_fd, "SENSOR FAIL: GYRO CAL ID"); return false; } int ret = ioctl(fd, GYROIOCSELFTEST, 0); if (ret != OK) { warnx("gyro self test failed"); mavlink_log_critical(mavlink_fd, "SENSOR FAIL: GYRO CHECK/CAL"); return false; } close(fd); return true; } static bool baroCheck(int mavlink_fd) { int fd = open(BARO0_DEVICE_PATH, 0); if(fd < 0) { mavlink_log_critical(mavlink_fd, "SENSOR FAIL: Barometer"); return false; } close(fd); return true; } bool preflightCheck(int mavlink_fd, bool checkMag, bool checkAcc, bool checkGyro, bool checkBaro, bool checkRC) { //give the system some time to sample the sensors in the background usleep(150000); //Magnetometer if(checkMag) { if(!magnometerCheck(mavlink_fd)) { return false; } } //Accelerometer if(checkAcc) { if(!accelerometerCheck(mavlink_fd)) { return false; } } // ---- GYRO ---- if(checkGyro) { if(!gyroCheck(mavlink_fd)) { return false; } } // ---- BARO ---- if(checkBaro) { if(!baroCheck(mavlink_fd)) { return false; } } // ---- RC CALIBRATION ---- if(checkRC) { if(rc_calibration_check(mavlink_fd) != OK) { return false; } } //All is good! return true; } }